CA2488316A1 - Systeme de gestion thermique pour aeronef - Google Patents

Systeme de gestion thermique pour aeronef Download PDF

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Publication number
CA2488316A1
CA2488316A1 CA002488316A CA2488316A CA2488316A1 CA 2488316 A1 CA2488316 A1 CA 2488316A1 CA 002488316 A CA002488316 A CA 002488316A CA 2488316 A CA2488316 A CA 2488316A CA 2488316 A1 CA2488316 A1 CA 2488316A1
Authority
CA
Canada
Prior art keywords
fuel
high temperature
management system
thermal management
oil
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002488316A
Other languages
English (en)
Other versions
CA2488316C (fr
Inventor
Daniel Sabatino
Louis J. Spadaccini
Scott Kaslusky
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of CA2488316A1 publication Critical patent/CA2488316A1/fr
Application granted granted Critical
Publication of CA2488316C publication Critical patent/CA2488316C/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/34—Conditioning fuel, e.g. heating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Liquid Carbonaceous Fuels (AREA)
CA002488316A 2004-01-20 2004-11-23 Systeme de gestion thermique pour aeronef Expired - Fee Related CA2488316C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/760,663 US7260926B2 (en) 2004-01-20 2004-01-20 Thermal management system for an aircraft
US10/760,663 2004-01-20

Publications (2)

Publication Number Publication Date
CA2488316A1 true CA2488316A1 (fr) 2005-07-20
CA2488316C CA2488316C (fr) 2008-02-05

Family

ID=34634558

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002488316A Expired - Fee Related CA2488316C (fr) 2004-01-20 2004-11-23 Systeme de gestion thermique pour aeronef

Country Status (6)

Country Link
US (1) US7260926B2 (fr)
EP (1) EP1557357B1 (fr)
JP (1) JP2005207415A (fr)
KR (1) KR100688415B1 (fr)
CN (1) CN1644892A (fr)
CA (1) CA2488316C (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111794864A (zh) * 2019-04-05 2020-10-20 通用电气公司 泵混合器分离器单元

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US10941706B2 (en) 2018-02-13 2021-03-09 General Electric Company Closed cycle heat engine for a gas turbine engine
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US11193671B2 (en) 2018-11-02 2021-12-07 General Electric Company Fuel oxygen conversion unit with a fuel gas separator
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US11319085B2 (en) 2018-11-02 2022-05-03 General Electric Company Fuel oxygen conversion unit with valve control
US11577852B2 (en) 2018-11-02 2023-02-14 General Electric Company Fuel oxygen conversion unit
US11161622B2 (en) 2018-11-02 2021-11-02 General Electric Company Fuel oxygen reduction unit
US11131256B2 (en) 2018-11-02 2021-09-28 General Electric Company Fuel oxygen conversion unit with a fuel/gas separator
US11148824B2 (en) 2018-11-02 2021-10-19 General Electric Company Fuel delivery system having a fuel oxygen reduction unit
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CN109515728B (zh) * 2018-11-08 2021-03-09 北京航空航天大学 带有辅助热油箱回路的飞机热管理***和方法
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CN111794864A (zh) * 2019-04-05 2020-10-20 通用电气公司 泵混合器分离器单元
CN111794864B (zh) * 2019-04-05 2023-08-04 通用电气公司 泵混合器分离器单元
US12025054B2 (en) 2019-04-05 2024-07-02 General Electric Company Pump mixer separator unit

Also Published As

Publication number Publication date
US7260926B2 (en) 2007-08-28
EP1557357A3 (fr) 2008-04-23
CN1644892A (zh) 2005-07-27
EP1557357B1 (fr) 2014-10-29
US20050155353A1 (en) 2005-07-21
CA2488316C (fr) 2008-02-05
EP1557357A2 (fr) 2005-07-27
JP2005207415A (ja) 2005-08-04
KR100688415B1 (ko) 2007-03-02
KR20050076595A (ko) 2005-07-26

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